13122 Federal Register / Vol. 73, No. 49 / Wednesday, March 12, 2008 / Rules and Regulations 

Compliance 

(e) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Detailed Inspection 

(f) Before the accumulation of 8,600 total 

flight cycles, or within 1,100 flight cycles 

after the effective date of this AD, whichever 

occurs later: Perform a detailed inspection to 

detect cracking of the left side and right side 

frames and reinforcement angles at FS640 

between stringer 9 and stringer 12, in 

accordance with Part A of the 

Accomplishment Instructions of Bombardier 

Service Bulletin 601R–53–061, Revision E, 

dated December 7, 2006. 

Note 1: For the purposes of this AD, a 

detailed inspection is: ‘‘An intensive 

examination of a specific item, installation, 

or assembly to detect damage, failure, or 

irregularity. Available lighting is normally 

supplemented with a direct source of good 

lighting at an intensity deemed appropriate. 

Inspection aids such as mirror, magnifying 

lenses, etc., may be necessary. Surface 

cleaning and elaborate procedures may be 

required.’’

Repetitive Inspection and Corrective Action 

(g) If no crack is found during the 

inspection required by paragraph (f) of this 

AD: Repeat the detailed inspection thereafter 

at intervals not to exceed 1,100 flight cycles, 

until the frame modification described in 

paragraph (h)(2) of this AD or the optional 

terminating modification described in 

paragraph (i) of this AD has been done. 

(h) If any crack is found during the 

inspection required by paragraph (g) of this 

AD: Before further flight, repair the crack in 

accordance with paragraph (h)(1), (h)(2), or 

(h)(3) of this AD, as applicable. 

(1) For any crack found in the frame at the 

stringer 9 cut-out only, repair in accordance 

with Part A of the Accomplishment 

Instructions of Bombardier Service Bulletin 

601R–53–061, Revision E, dated December 7, 

2006. 

(2) For any crack found in the frame 

reinforcement doubler only, do the actions 

described in paragraphs (h)(2)(i) and (h)(2)(ii) 

of this AD. 

(i) Do the frame modification (including 

related investigative and corrective actions) 

described in Part C of the Accomplishment 

Instructions of Bombardier Service Bulletin 

601R–53–061, Revision E, dated December 7, 

2006; except where the service bulletin 

specifies to contact the manufacturer for 

repair instructions, repair the crack using a 

method approved by either the Manager, 

New York Aircraft Certification Office (ACO), 

FAA; or Transport Canada Civil Aviation 

(TCCA) (or its delegated agent). 

(ii) Within 12,000 flight cycles after doing 

the modification required by paragraph 

(h)(2)(i) of this AD, do the detailed inspection 

required by paragraph (f) of this AD, then 

repeat the detailed inspection thereafter at 

intervals not to exceed 1,100 flight cycles. 

(3) For any crack found in areas of the 

inspection zone described in paragraph (f) of 

this AD other than those areas described in 

paragraphs (h)(1) and (h)(2) of this AD: 

Repair the crack using a method approved by 

either the Manager, New York ACO, FAA; or 

TCCA (or its delegated agent). 

Optional Terminating Action 

(i) Reinforcement of any engine support 

beam in accordance with the 

Accomplishment Instructions of the service 

information described in paragraph (i)(1) or 

(i)(2) of this AD, as applicable, ends all 

repetitive inspections required by this AD for 

that support beam. 

(1) For all airplanes: If the reinforcement is 

done before the effective date of this AD, 

Bombardier Alert Service Bulletin A601R–

53–059, Revision E, dated March 21, 2005; or 

Revision F, dated April 21, 2006; may be 

used. After the effective date of this AD, only 

Bombardier Alert Service Bulletin A601R–

53–059, Revision F, may be used. 

(2) For airplanes identified in Bombardier 

Service Bulletin 601R–53–065, Revision B, 

dated November 2, 2007: If the reinforcement 

is done before the effective date of this AD, 

Bombardier Service Bulletin 601R–53–065, 

Revision A, dated August 24, 2005, or 

Revision B, may be used. After the effective 

date of this AD, only Bombardier Service 

Bulletin 601R–53–065, Revision B, may be 

used. 

No Reporting Requirement 

(j) Although Bombardier Service Bulletin 

601R–53–061, Revision E, dated December 7, 

2006, specifies to submit certain information 

to the manufacturer, this AD does not 

include that requirement. 

Alternative Methods of Compliance 

(AMOCs) 

(k)(1) The Manager, New York ACO, FAA, 

has the authority to approve AMOCs for this 

AD, if requested in accordance with the 

procedures found in 14 CFR 39.19. 

(2) To request a different method of 

compliance or a different compliance time 

for this AD, follow the procedures in 14 CFR 

39.19. Before using any approved AMOC on 

any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

Related Information 

(l) Canadian airworthiness directive CF–

2003–12, dated May 7, 2003, also addresses 

the subject of this AD. 

Material Incorporated by Reference 

(m) You must use Bombardier Service 

Bulletin 601R–53–061, Revision E, dated 

December 7, 2006, including Appendix B, 

Revision C, dated June 25, 2003, to do the 

actions required by this AD, unless the AD 

specifies otherwise. If you accomplish the 

optional actions specified by this AD, you 

must use Bombardier Alert Service Bulletin 

A601R–53–059, Revision F, dated April 21, 

2006, excluding Appendix A, dated June 14, 

2001; or Bombardier Service Bulletin 601R–

53–065, Revision B, dated November 2, 2007; 

as applicable; to perform those actions, 

unless the AD specifies otherwise. 

Bombardier Service Bulletin 601R–53–061, 

Revision E, dated December 7, 2006, includes 

the following effective pages: 

Page Nos. 

Revision 

level 

shown on 

page 

Date shown on 

page 

1–44 ........... E December 7, 

2006. 

Appendix B 

B1–B8 ........ C June 25, 2003. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Bombardier, Inc., Canadair, 

Aerospace Group, P.O. Box 6087, Station 

Centre-ville, Montreal, Quebec H3C 3G9, 

Canada. 

(3) You may review copies of the service 

information incorporated by reference at the 

FAA, Transport Airplane Directorate, 1601 

Lind Avenue, SW., Renton, Washington; or at 

the National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http:// 

www.archives.gov/federal_register/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on March 3, 

2008. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E8–4644 Filed 3–11–08; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2007–28529; Airspace 

Docket No. 07–ANM–12] 

Modification of Class E Airspace; 

Tucson, AZ 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action will modify Class 

E airspace at Tucson, AZ. Additional 

controlled airspace is necessary to 

encompass holding patterns and 

intermediate segments at Tucson 

International Airport. The FAA is 

proposing this action to enhance the 

safety and management of Instrument 

Flight Rules (IFR) operations at Tucson 

International Airport, Tucson, AZ. 

DATES: Effective Date: 0901 UTC, June 5, 

2008. The Director of the Federal 

Register approves this incorporation by 

reference action under 1 CFR part 51, 

subject to the annual revision of FAA 


jlentini on PROD1PC65 with RULES
Federal Register / Vol. 73, No. 49 / Wednesday, March 12, 2008 / Rules and Regulations 13123 

Order 7400.9 and publication of 

conforming amendments. 

FOR FURTHER INFORMATION CONTACT: 

Richard Roberts, Federal Aviation 

Administration, System Support Group, 

Western Service Area, 1601 Lind 

Avenue, SW., Renton, WA, 98057; 

telephone (425) 203–4517. 

SUPPLEMENTARY INFORMATION: 

History 

On August 29, 2007 the FAA 

published in the Federal Register a 

notice of proposed rulemaking to 

modify Class E airspace at Tucson, AZ 

(72 FR 49677). This action would 

enhance the safety and management of 

Instrument Flight Rules (IFR) operations 

at Tucson International Airport, Tucson, 

AZ. 

Interested parties were invited to 

participate in this rulemaking effort by 

submitting written comments on the 

proposal to the FAA. No comments 

were received. 

Class E airspace designations are 

published in paragraph 6005 of FAA 

Order 7400.9R signed August 15, 2007, 

and effective September 15, 2007, which 

is incorporated by reference in 14 CFR 

part 71.1. The Class E airspace 

designations listed in this document 

will be published subsequently in that 

Order. 

The Rule 

This action amends Title 14 Code of 

Federal Regulations (14 CFR) part 71 by 

modifying Class E airspace at Tucson 

International Airport, Tucson, AZ. 

Additional controlled airspace is 

necessary to encompass hold-in-lieu 

patterns at the LIPTE Initial Fix/ 

Instrument Approach Fix (IF/IAF) at 

Tucson International Airport, Tucson, 

AZ and encompass intermediate 

segments from the ILEEN Distance 

Measuring Equipment (DME) fix to 

COPEY DME fix. The FAA is proposing 

this action to enhance the safety and 

management of IFR operations at 

Tucson International Airport, Tucson, 

AZ. 

The FAA has determined that this 

regulation only involves an established 

body of technical regulations for which 

frequent and routine amendments are 

necessary to keep them operationally 

current. Therefore, this regulation: (1) Is 

not a ‘‘significant regulatory action’’

under Executive Order 12866; (2) is not 

a ‘‘significant rule’’ under DOT 

Regulatory Policies and Procedures (44 

FR 11034; February 26, 1979); and (3) 

does not warrant preparation of a 

regulatory evaluation as the anticipated 

impact is so minimal. Since this is a 

routine matter that will only affect air 

traffic procedures and air navigation, it 

is certified that this rule, when 

promulgated, will not have a significant 

economic impact on a substantial 

number of small entities under the 

criteria of the Regulatory Flexibility Act. 

This rulemaking is promulgated under 

the authority described in Subtitle VII, 

Part A, Subpart I, Section 40103. Under 

that section, the FAA is charged with 

prescribing regulations to assign the use 

of airspace necessary to ensure the 

safety of aircraft and the efficient use of 

airspace. This regulation is within the 

scope of that authority as it modifies 

controlled airspace at Tucson 

International Airport, Tucson, AZ. 

List of Subjects in 14 CFR Part 71 

Airspace, Incorporation by reference, 

Navigation (air) 

Adoption of the Amendment 

■ In consideration of the foregoing, the 

Federal Aviation Administration 

amends 14 CFR part 71 as follows: 

PART 71—DESIGNATION OF CLASS A, 

B, C, D, AND E AIRSPACE AREAS; AIR 

TRAFFIC SERVICE ROUTES; AND 

REPORTING POINTS 

■ 1. The authority citation for 14 CFR 

part 71 continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40103, 40113, 

40120; E. O. 10854, 24 FR 9565, 3 CFR, 1959–

1963 Comp., p. 389. 

§ 71.1 [Amended] 

■ 2. The incorporation by reference in 

14 CFR 71.1 of the Federal Aviation 

Administration Order 7400.9R, Airspace 

Designations and Reporting Points, 

signed August 15, 2007, and effective 

September 15, 2007 is amended as 

follows: 

Paragraph 6005. Class E airspace areas 

extending upward from 700 feet or more 

above the surface of the earth. 

* * * * * 

AWP AZ E5 Tucson, AZ 2 spaces 

[Modified] 

Tucson International Airport, AZ 

(Lat. 32°06′58′′ N, long. 110°56′28′′ W) 

Ryan Field, AZ 

(Lat. 32°08′32′′ N, long. 111°10′28′′ W) 

That airspace extending upward from 

700 feet above the surface within an 8.7- 

mile radius of Tucson International 

Airport and within that airspace 

bounded by a line beginning at lat. 

32°11′01′′ N, long. 111°05′33′′ W; to lat. 

32°21′28′′ N, long. 111°16′33′′ W; to lat. 

32°35′55′′ N, long. 110°57′47′′ W; to lat. 

32°01′35′′ N, long. 110°21′18′′ W; to 

lat.31°44′6′′ N, long. 110°42′30′′ W; to 

lat.31°58′20′′ N, long. 110°57′51′′ W; to 

intercept the 8.7-mile radius southwest 

of the Tucson International Airport; 

thence clockwise via the 8.7-mile radius 

to the point of beginning; and that 

airspace within a 4.3-mile radius of 

Ryan Field and within 3.5 mile each 

side of the Ryan Field localizer course 

extending from the 4.3-mile radius to 7 

miles west of the outer marker. That 

airspace extending upward from 1,200 

feet above the surface bounded by a line 

beginning at lat. 32°33′00′′ N, long. 

111°45′02′′ W; to lat.32°33′00′′ N, long. 

110°52′02′′ W; thence north via long. 

110°52′00′′ W; to the south boundary of 

V–94, thence southeast via the south 

boundary of V–94; to long. 110°00′02′′ 

W, thence south to lat. 31°39′00′′ N; long 

110°00′02′′ W; to lat. 31°39′00′′ N, long. 

111°00′02′′ W; to lat. 32°00′00′′ N, long. 

111°45′02′′ W, to the point of origin. 

* * * * * 

Issued in Seattle, Washington, on February 

28, 2008. 

Kevin Nolan, 

Acting Manager, System Support Group, 

Western Service Center. 

[FR Doc. 08–996 Filed 3–11–08; 8:45 am] 

BILLING CODE 4910–13–M 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 111 

[Docket No. FDA–2008–N–0152] (formerly 

Docket No. 1996N–0417) 

RIN 0910–AB88 

Current Good Manufacturing Practice 

in Manufacturing, Packaging, Labeling, 

or Holding Operations for Dietary 

Supplements; Technical Amendment 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; technical 

amendment. 

SUMMARY: The Food and Drug 

Administration (FDA) is correcting a 

final rule that appeared in the Federal 

Register of June 25, 2007 (72 FR 34752). 

The final rule established current good 

manufacturing practice (CGMP) 

requirements in manufacturing, 

packaging, labeling, or holding 

operations for dietary supplements. The 

final rule was published with an 

inadvertent error in the codified section. 

This document corrects that error. This 

action is being taken to improve the 

accuracy of the agency’s regulations. 

DATES: This rule is effective March 12, 

2008. 

FOR FURTHER INFORMATION CONTACT: 

Vasilios H. Frankos, Center for Food 


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